Analogue Computers For Vehicles TRIZ Cases

A boat engine control unit adjusts fuel injection and ignition timing using predicted speed values derived from intake pressure and rotational signals.

A routing tool processes flight and geographic data to generate route data for safe off-airport landing areas.

A remote control side ECU processes rotational speed change commands before transmitting periodic signals to an engine side unit.

A landing gear monitor measures hydraulic fluid pressure in the main strut to evaluate peak loads during bogie wheel contact modes.

System segments personal vehicle costs into distinct components to resolve calculation accuracy versus complexity trade-offs for travelers.

A vehicle fuel consumption meter displays instantaneous and average fuel data using a swinging pointer to show deviation from a reference state.

A vehicle group forming device selects and orders vehicles based on their conformity to priority lane traveling conditions.

Aircraft navigation monitoring system displays achievable height parameters alongside setpoint values to provide pilots with real-time performance data.

A traffic information collecting digital map matches GPS probe data against discrete detection nodes spaced at predetermined intervals.

A diagnostic control system monitors engine knock signals to identify discrete variable valve lift faults in specific cylinders.

An exhaust pressure sensor detects valve opening after deactivation to monitor cylinder status.

A knock control apparatus calculates intensity variance and standard deviation to set a dynamic determination level.

Microprocessor-controlled switching element ensures reliable engine shutdown despite wire breakage in traditional direct-grounding circuits.

Dynamic acceleration limits reduce fuel consumption during light loads while preserving vehicle performance under heavy conditions.

A virtual loading element simulates tire tread displacement to determine loaded wheel non-uniformities via outer contour scanning.

A vehicle performance monitoring system calculates engine horsepower and fuel consumption using sensor signals and stored maps.

An accelerometer-based ground-sensing ball measures impact dynamics to classify surfaces, replacing heavy terramechanics systems with a lightweight payload.

A fuel injection control system detects the minimum interval between adjacent injection periods to learn actuator displacement deviations.

Calculating capture zone width based on altitude and speed optimizes vertical acceleration limits, ensuring passenger comfort during descent.

Hierarchical segmentation divides processing between high-power and low-power controllers, reducing energy consumption while maintaining measurement precision.

Synchronizes operation amount calculations with crank angle signals to shorten control delay times and improve valve timing accuracy.

Estimating fresh air charge pressure enables fault detection for the EGR valve, resolving control precision issues during HCCI combustion.

A hybrid vehicle creep control system adjusts motor driving based on inter-vehicle distance to maintain stable spacing.

An exhaust gas recirculation valve uses bypassed hot gas to oxidize soot and hydrocarbon deposits on internal surfaces.

Gain switching unit adjusts amplification to maximize AD conversion dynamic range.

Parallel monitoring circuits validate drive commands without interrupting operation, maintaining reliability.

Control device schedules late partial injections within setpoint crankshaft angle ranges to avoid temporal overlaps and reduce power losses.

A vehicle-mounted device merges dispatching and navigation modules to automate route calculation for taxi drivers.

A wireless data collection unit converts pulse signals from fueling operations into volumetric totals using software configurable hardware filters.

Dual exhaust probes and trim controllers decouple diagnostic signals from trim control, resolving asymmetric response issues during catalytic converter testing.

Dynamic exhaust control signals prevent ammonia slip by balancing NOx conversion against excess urea injection.

A radar traffic sensor uses a planar antenna plate and transceiver circuit to detect vehicles via microwave signals.

Segments total battery energy consumption to exclude air conditioning usage, improving distance to empty estimation accuracy.

Electronic flight control system adjusts rotor speeds based on pilot commands and automatic flight tables.

Frequency span analysis resolves adjacent lane interference by mapping vehicle detection to specific lanes, improving boundary identification accuracy.

Controller segments engines by response time, switching between fast and high-capacity groups to reduce adaptation delays.

A controller calculates engine rotation speed using crankshaft angular acceleration near combustion top dead center.

A driving amount controller adjusts motor damping output based on throttle valve opening deviation to enhance response performance.

An engine control apparatus selects operating modes using mode maps to set target torque based on accelerator opening and engine speed.

An auxiliary flight management system integrates mission-specific graphical data into primary flight plans to display specialized symbology.

A digital camera system analyzes partial image data to determine vehicle presence and right-of-way for adaptive traffic signal control.

Vehicles transmit energy consumption and location data to a central processor for route optimization.

A display system renders missed approach procedure legs and varies visual characteristics based on aircraft position.

A volatile memory backup mechanism validates stored change history data after power restoration to maintain accurate engine valve lift calculations.

A vehicle fuel informational system monitors fuel levels and suggests nearby providers using onboard positioning data.

A dual communication interface system segments high-speed development data transfer from real-time vehicle function unit communication.

A misfire detecting device distinguishes intentional control misfires from abnormal engine faults in water jet propulsion systems.

A trusted link synchronizes portable electronic flight bag devices with installed aircraft systems.